Douglas DC-9-31

Service difficulty reports · 7,433

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC931'
  ORDER BY difficulty_date DESC"

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SDR TWAA9904010Window · damagedDURING OP 16 MAINT CHECK, FOUND STATIC BURN ON CABIN WINDOW NR 36 ON LT SIDE OF AIRCRAFT, AFT EDGE AND FWD EDGE OF WINDOW. BLENDED PER SRM 53-05, FIG 3. INSTALLED DOUBLER PER DRAWING SRO9530053, AND ARA 16105.Mar 10, 1999 · N987Z · Doug DC931 · Passenger Compartment WindowsSDR TWAA9903905Window · damagedDURING OP 16 MAINT CHECK, FOUND STATIC BURN ON CABIN WINDOWS ON LEFT SIDE OF CABIN NUMBERS 31 AND 32. BLENDED PER SRM 53-05 FIG III. REPAIRED PER ARA 16114A AND SERVICE REPAIR DRAWING SR09530053.Mar 10, 1999 · N987Z · Doug DC931 · Passenger Compartment WindowsSDR 9900869959Battery Pack · dischargedDURING LINE MAINTENANCE INSPECTION, FOUND CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT TAIL COMPARTMENT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK NORMAL.Mar 9, 1999 · N919RW · Doug DC931 · Emergency LightingSDR USAAD99039Battery · dischargedIND - THE LEFT NACELLE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE LEFT NACELLE EMERGENCY LIGHT BATTERY. (M)Mar 8, 1999 · N920VJ · Doug DC931 · Emergency LightingSDR USAA990249Pan · damagedPIT - DURING RON VISIT FOUND .25 INCH TO .375 INCH HOLE IN SERVICE DOOR HOLD OPEN PAN ASSEMBLY RIGHT SIDE OF FUSELAGE. INSTALLED NEW PAN ASSEMBLY PER EA 51678. (M)Mar 8, 1999 · N929VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9903906Support · corrodedDURING OP 16 MAINT CHECK, FOUND FLOOR SUPPORT CORRODED TOP AND BOTTOM SIDES AT STA 160 TO 200, RBL 44 IN. REPLACED PART PER SPM 6-70-1 AR 2 FROM STA 160 TO 200.Mar 8, 1999 · N987Z · Doug DC931 · Fuselage Main, Floor BeamSDR TWAA9903703Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOOR SUPPORTS AT STA 200 RBL 22 IN TO 42 IN, STA 160 TO 200 RBL 44 IN, STA 160 TO 200 LBL 54 IN, STA 200 RBL 44 TO 55, STA 200 LBL 0 TO 20, AND STA 180 RBL 1 TO 44. REPLACED AFFECTED FLOOR SUPPORTS PER SPM 6Mar 8, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9903810Support · corrodedDURING OP 16 MAINT CHECK, FOUND CENTER CABIN FLOOR CENTER SUPPORT BEAM WITH CORROSION AT STA 218. REPLACED FLOORBEAM PER SPM 6-70-01, USING ORIGINAL TYPE HARDWARE, STA 160 TO 218.Mar 7, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9903809Longeron · wornDURING OP 16 MAINT CHECK, FOUND A HOLE WORN IN LONGERON 8L AT STA 1066. REPLACED LONGERON FROM STA 1065 TO 1087. SPLICED PER SRM 53-02 FIG 18.Mar 7, 1999 · N987Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990191Jamb · crackedPIT - DURING RON VISIT, FOUND 6 INCH CRACK AT STATION Z53.625 DOOR JAMB, AFT PAX LEFT SIDE. INSTALLED REPAIR ANGLE PER EA 51672. (M)Mar 6, 1999 · N955VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9900034Bulb · failedDTW - EMERGENCY FLOOR TRACK LIGHTS. FIRST LIGHT MISSING BULB AND COVER. REPLACED BULB AND COVER. OPERATION CHECKS GOOD. (M)Mar 6, 1999 · N969ML · Doug DC931 · Emergency LightingSDR USAA990222Support · corrodedPIT - DURING Q-1 CHECK, FOUND RIGHT LAV CENTER FLOOR SUPPORT CORRODED AND CRACKED .75 INCH AT STATION 965. CORROSION LEVEL 1, CORROSION TASK NR C58-5330. CLEANED CORROSION, TREATED AND PRIMED PER SRM. MANUFACTURED NEW FLOOR SUPPORT TAB FROM 7075-T6.040 PER Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990201Jamb · damagedPIT - DURING Q-1 CHECK, FOUND SMALL HOLE IN AFT CARGO DOOR JAMB WEB JUST ABOVE 29 RIGHT. REMOVED DAMAGED SECTION OF WEB, MANUFACTURED NEW WEB PIECE FROM C/C 109-5712. MADE SPLICES FROM 7075-T6 .050 INCH AND INSTALLED PER EA NR 51599. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990200Frame · crackedPIT - DURING Q-1 CHECK, FOUND .5 INCH LENGTH BY .21875 INCH WIDE BY .019 INCH DEEP CHAFE IN FRAME NR 1059 LONGERON 15L. INSTALLED DOUBLER PER SRM 53-01, FIG 2 SHEET 4 AND EA 51616. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990199Cusp · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK IN CUSP MEMBRANE LEFT BETWEEN STATION NR 935 AND 945. FABRICATED CUSP MEMBRANE AND INSTALLED PER EA 51628. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990198Bracket · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK ON TAIL INTERIOR ON VERTICAL ATTACH BRACKET FOR 'Y' DUT STATION 1087 BELOW 5R. REPLACED DEFECTIVE PART WITH IDENTICAL PART NUMBER. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990197Frame · chafedPIT - DURING Q-1 CHECK, FOUND CHAF .372 INCH BY .196 INCH WIDE BY .029 INCH DEEP AT FRAME 1019 BELOW LONGERON 13R. CUT OUT DAMAGE AREA OF FRAME AND SPLICED IN A NEW SECTION OF FRAME AND SPLICED IN A NEW SECTION OF FRAME PER SRM 53-03 FIG 4. (M0Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990196Cusp · crackedPIT - DURING Q-1 CHECK, FOUND CRACKS 1.75 AND 3.5 INCH LEFT SIDE OF CABIN STATION 598 CUSP MEMBRANE. CUT OUT AND INSTALLED NEW SECTION PER EA 51628. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990195Intercostal · crackedPIT - DURING Q-1 CHECK, FUOND 1.25 INCH CRACK IN INTERCOSTAL BETWEEN CABIN FLOORBEAMS NR 965-980, C/L OF A/C UPPER FLANGE. INSTALLED DOUBLER MANUFACTURED FROM 7075T6 .032 INCH PER SRM 53-01, FIG 2. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990194Strap · corrodedPIT - DURING Q-1 CHECK, FOUND CORROSION ON CARGO TIE DOWN STRAP .75 INCH DIAMETER BY .008 DEEP AT LEFT SIDE BETWEEN STATION 897-925 ON STRAP. CORROSION LEVEL 1, CORROSION TASK NR C57-53300. SPLICED IN NEW PART MANUFACTURED SPLICE ANGLES AND INSTALLED PER DRAMar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990193Support · corrodedPIT - DURING Q-1 CHECK, FOUND 41.5 INCH LONG, LEVEL 1 CORROSION AT ENTRANCE FLOOR SUPPORT 39 EXTRUSION, LIGHT CORROSION FULL LENGTH. CORROSION LEVEL 1, CORROSION TASK NR C46-53303. REPLACED SUPPORT WITH MODIFIED PART NR 992348429. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990192Support · corrodedPIT - DURING Q-1 CHECK, FUOND 4.5 INCH LONG, LEVEL 1 CORROSION AT ENTRANCE FLOOR SUPPORT 23 EXTRUSION, LIGHT CORROSION FULL LENGTH. CORROSION LEVEL 1, CORROSION TASK NR C46-533013. REPLACED SUPPORT WITH MODIFIED PART NR S265247912000. (M)Mar 5, 1999 · N919VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990190Skin · crackedPIT - DURING MAINTENANCE WALK AROUND, FOUND 3 INCH CRACK AND 9 INCH VERTICAL CRACK ON FUSELAGE SKIN BETWEEN STATION 1155.335 AND STATION 1168.895 LEFT SIDE. INSTALLED EXTERNAL DOUBLER, CUTOUT DAMAGE PER SRM 53-04 FIG 12B CLASS II REPAIR. (M)Mar 5, 1999 · N913VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9903808Former · wornDURING OP 16 MAINT CHECK, FOUND IN AFT ACCESSORY COMPT A FORMER AT STA 1059 WITH A WORN AREA AT LONGERON 8L. REPAIRED WORN AREA IN FORMER RING PER SRM 53-03, FIG 4.Mar 5, 1999 · N987Z · Doug DC931 · Fuselage Main, FrameSDR 9900929963Skin · crackedDURING PERIODIC CHECK, FOUND CRACKS AT FS 69 BETWEEN LONGERONS 15R AND 20R AND AT FS 76 BETWEEN LONGERONS 15R AND 21R. INSTALLED REPAIRS PER EA 99-165600.Mar 5, 1999 · N913RW · Doug DC931 · Fuselage Main, Plate/SkinSDR 9900919963Frame · crackedDURING PERIODIC CHECK, FOUND CRACK IN FRAME AT LONGERON 12R, FS 69.5. INSTALLED REPAIR PER EA 99-162-56.Mar 5, 1999 · N913RW · Doug DC931 · Fuselage Main, FrameSDR USAAD99037Battery Pack · dischargedCMH - THE MID CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE MID CABIN CEILING EMERGENCY LIGHT POWER SUPPLY. (M)Mar 4, 1999 · N935VJ · Doug DC931 · Emergency LightingSDR TWAA9903807Longeron · crackedDURING OP 16 MAINT CHECK, FOUND LONGERON CRACKED AT ATTACH TO FORMER RING STA 160, LONGERON 3L. REPLACED LONGERON FROM STA 160 TO 170 WITH NEW LONGERON SPLICE PER SRM 53-02 PAGE 48 AND SPM 6-70-01, FASTENERS PER 51-30-0.Mar 4, 1999 · N987Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAAD99036Battery · dischargedIND - THE EMERGENCY LIGHTS AFT OF ROW 19 AND THE LIGHT ABOVE THE AFT FLIGHT ATTENDANT SEAT WERE INOPERATIVE. MAINTENANCE REPLACED THE NECESSARY EMERGENCY LIGHT BATTERIES. (M)Mar 3, 1999 · N959VJ · Doug DC931 · Emergency LightingSDR TWAA9903813Seat Track · wornDURING OP 16 FOUND CHAIR TRACK NR 3 BLENDED OUT OF LIMITS AT STA 266, APPROX 22 IN LBL. INSTALLED NEW TRACK SPLICED IN AT STA 266 TO STA 198. SPLICED PER SEAT TRACK SPLICE REPAIR SRM 53-05 PG 7 FIG 4, SHEET 1.Mar 3, 1999 · N987Z · Doug DC931 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9903811Longeron · wornDURING OP 16 MAINT CHECK, FOUND AFT ACCY COMPT WITH WORN AREA ON LONGERON 8R AT STA 1065. REPAIRED WORN AREA IN LONGERON 8R AT STA 1065 WITH A SPLICE REPAIR PER SRM 53-02.Mar 3, 1999 · N987Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9903806Web · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION IN LT WHEEL WELL UNDER FWD SIDE OF OVERHEAD LIGHT. REMOVED SURFACE CORROSION PER SPM 6-80-01.Mar 3, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9903805Tee Cap · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON TEE CAP AT STA 699, APPROX 58.2 IN ON SLANTED PANEL. MECHANICALLY REMOVED CORROSION PER TWA STD PROCESSES 6-80-01.Mar 3, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR 9900849943Valve · leakingLOSS OF RIGHT HYDRAULIC SYSTEM QUANTITY AND PRESSURE OCCURRED AFTER TAKEOFF. CREW DECLARED AN EMERGENCY AND FLIGHT WAS RETURNED TO DFW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING HYDRAULIC FLOW CONTROL VALVE. LEAK CHECK WAS GOOD. AIRMar 3, 1999 · N1308T · Doug DC931 · Hydraulic System, MainSDR USAAD99034Control Box · failedPIT-SBN - FLT 753 - AFTER TAKEOFF, THE RIGHT MLG UNSAFE LIGHT ILLUMINATED WITH THE GEAR HANDLE UP. THE LANDING WAS CYCLED BUT THE LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PROXIMITY SENSING CMar 2, 1999 · N924VJ · Doug DC931 · Landing Gear Position and WarningSDR TWAA9903812Panel · crackedDURING OP 16 MAINT CHECK, FOUND IN NLG WHEEL WELL AN 8 INCH CRACK IN THE WW LOWER SURFACE OF CANTED PRESSURE PANEL, 2 IN FWD OF E & E DOOR. REMOVED AND REPLACED Y CHORD ANGLE PER DOUGLAS PRINT 9911500.Mar 2, 1999 · N987Z · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900156Latch · looseCOCKPIT DOOR WOULD NOT OPEN FROM CABIN. LATCH SLIPPED. SECURED DOOR KNOB LATCH SCREW.Mar 2, 1999 · N943AX · Doug DC931 · Fixed Inner DoorsSDR USAAD99033Power Supply · failedIND - THE RIGHT EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE RIGHT EXTERIOR EMERGENCY LIGHT POWER SUPPLY. (M)Mar 1, 1999 · N958VJ · Doug DC931 · Emergency LightingSDR USAAD99032Battery Charger · failedIND - THE AFT SECTION OF THE FLOOR TRACK EMERGENCY LIGHTS WAS INOPERATIVE. MAINTENANCE REPLACED THE AFT FLOOR TRACK EMERGENCY LIGHT BATTERY CHARGER. (M)Feb 28, 1999 · N982VJ · Doug DC931 · Emergency LightingSDR USAAD99031Battery · dischargedIND - THE RIGHT NACELLE EMERGENCY LIGHT AND TWO SECTIONS OF THE CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE INOPERATIVE LIGHTS. (M)Feb 28, 1999 · N937VJ · Doug DC931 · Emergency LightingSDR 99ZZZM230Battery · dischargedIND - THE RIGHT NACELLE EMERGENCY LIGHT AND TWO SECTIONS OF THE CABIN CEILING EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE INOPERATIVE LIGHTS. (M)Feb 28, 1999 · N937VJ · Doug DC931 · Emergency LightingSDR 9900729952Bulb · failedDURING LINE MAINTENANCE INSPECTION, FOUND TAIL CONE EMERGENCY LIGHTS INOPERATIVE. RELAMPED BULBS, OPERATIONAL CHECK NORMAL.Feb 28, 1999 · N916RW · Doug DC931 · Emergency LightingSDR USAA990189Clip · crackedPIT - DURING Q-1 CHECK, FOUND .5 INCH CRACK IN SKIN CLIP STATION 945 BETWEEN LONGERON 15R AND 14R. REPLACED SKIN CLIP, NEW PART NR 1197928. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990163Longeron · crackedPIT - DURING Q-1 CHECK, FOUND .5 INCH CRACK LONGERON 15L AT HI-LOCK AT STATION 945. SPLICED IN SECTION OF LONGERON PER SRM 53-11-3. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990162Longeron · crackedPIT - DURING Q-1 CHECK, FOUND .5 INCH LONGERON CRACK AT HI-LOCK AT LONGERON 17L STATION 945. SPLICED IN SECTION OF LONGERON PER SRM 53-11-3. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990161Skin · crackedPIT - DURING Q-1 CHECK, FOUND 2 INCH CRACK ON SKIN 4 INCH FORWARD OF FS 1038 AT LONGERON 18L. INSTALLED DOUBLER REPAIR PER SRM 54-01 FIG 2 (4.5 INCH BY 4 INCH). (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA990160Floorbeam · corrodedPIT - DURING Q-1 CHECK, FOUND 2 INCH BY 1 INCH AREA OF CORROSION AT STATION 965 OUTBOARD SIDE OF LT LAV THRESHOLD SUPPORT FLOORBEAM. REMOVED CORRODED SECTION OF CAP ANGLE AND INSTALLED NEW SECTION AND REPAIR ANGLES PER TYPICAL REPAIR 53-10-14. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Fuselage Main, Floor BeamSDR USAA990159Door Pan · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK FORWARD LEFT EMERGENCY EXIT LOWER AFT DOOR PAN. STOP DRILLED AND INSTALLED DOUBLER PER SRM 52-20-03. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Emergency ExitsSDR USAA990158Door Pan · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK AFT RIGHT EMERGENCY EXIT TOP FORWARD DOOR PAN. STOP DRILLED AND INSTALLED DOUBLER PER SRM 52-20-03. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Emergency ExitsSDR USAA990157Door Pan · crackedPIT - DURING Q-1 CHECK, FOUND 1 INCH CRACK RIGHT FORWARD EMERGENCY EXIT TOP FORWARD DOOR PAN. STOP DRILLED AND INSTALLED DOUBLER PER SRM 52-20-03. (M)Feb 27, 1999 · N937VJ · Doug DC931 · Emergency Exits
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